Adding overPotentialFoam and overRhoSimpleFoam and tutorials

applications/solvers/basic/potentialFoam/overPotentialFoam/Make/files

+potentialFoam.C
+
+EXE = $(FOAM_APPBIN)/overPotentialFoam

applications/solvers/basic/potentialFoam/overPotentialFoam/Make/options

+EXE_INC = \
+    -I$(LIB_SRC)/finiteVolume/lnInclude \
+    -I$(LIB_SRC)/dynamicFvMesh/lnInclude \
+    -I$(LIB_SRC)/overset/lnInclude \
+    -I$(LIB_SRC)/meshTools/lnInclude \
+    -I$(LIB_SRC)/sampling/lnInclude
+
+EXE_LIBS = \
+    -lfiniteVolume \
+    -lmeshTools \
+    -lsampling \
+    -loverset

applications/solvers/basic/potentialFoam/overPotentialFoam/createControls.H

+const dictionary& potentialFlow
+(
+    mesh.solutionDict().subDict("potentialFlow")
+);
+
+const int nNonOrthCorr
+(
+    potentialFlow.lookupOrDefault<int>("nNonOrthogonalCorrectors", 0)
+);

applications/solvers/basic/potentialFoam/overPotentialFoam/createFields.H

+Info<< "Reading velocity field U\n" << endl;
+volVectorField U
+(
+    IOobject
+    (
+        "U",
+        runTime.timeName(),
+        mesh,
+        IOobject::MUST_READ,
+        IOobject::AUTO_WRITE
+    ),
+    mesh
+);
+
+// Initialise the velocity internal field to zero
+U = dimensionedVector("0", U.dimensions(), Zero);
+
+surfaceScalarField phi
+(
+    IOobject
+    (
+        "phi",
+        runTime.timeName(),
+        mesh,
+        IOobject::NO_READ,
+        IOobject::AUTO_WRITE
+    ),
+    fvc::flux(U)
+);
+
+if (args.optionFound("initialiseUBCs"))
+{
+    U.correctBoundaryConditions();
+    phi = fvc::flux(U);
+}
+
+
+// Construct a pressure field
+// If it is available read it otherwise construct from the velocity BCs
+// converting fixed-value BCs to zero-gradient and vice versa.
+word pName("p");
+
+// Update name of the pressure field from the command-line option
+args.optionReadIfPresent("pName", pName);
+
+// Infer the pressure BCs from the velocity
+wordList pBCTypes
+(
+    U.boundaryField().size(),
+    fixedValueFvPatchScalarField::typeName
+);
+
+forAll(U.boundaryField(), patchi)
+{
+    if (U.boundaryField()[patchi].fixesValue())
+    {
+        pBCTypes[patchi] = zeroGradientFvPatchScalarField::typeName;
+    }
+}
+
+// Note that registerObject is false for the pressure field. The pressure
+// field in this solver doesn't have a physical value during the solution.
+// It shouldn't be looked up and used by sub models or boundary conditions.
+Info<< "Constructing pressure field " << pName << nl << endl;
+volScalarField p
+(
+    IOobject
+    (
+        pName,
+        runTime.timeName(),
+        mesh,
+        IOobject::READ_IF_PRESENT,
+        IOobject::NO_WRITE,
+        false
+    ),
+    mesh,
+    dimensionedScalar(pName, sqr(dimVelocity), 0),
+    pBCTypes
+);
+
+// Infer the velocity potential BCs from the pressure
+wordList PhiBCTypes
+(
+    p.boundaryField().size(),
+    zeroGradientFvPatchScalarField::typeName
+);
+
+forAll(p.boundaryField(), patchi)
+{
+    if (p.boundaryField()[patchi].fixesValue())
+    {
+        PhiBCTypes[patchi] = fixedValueFvPatchScalarField::typeName;
+    }
+}
+
+Info<< "Constructing velocity potential field Phi\n" << endl;
+volScalarField Phi
+(
+    IOobject
+    (
+        "Phi",
+        runTime.timeName(),
+        mesh,
+        IOobject::READ_IF_PRESENT,
+        IOobject::NO_WRITE
+    ),
+    mesh,
+    dimensionedScalar("Phi", dimLength*dimVelocity, 0),
+    PhiBCTypes
+);
+
+label PhiRefCell = 0;
+scalar PhiRefValue = 0;
+setRefCell
+(
+    Phi,
+    potentialFlow.dict(),
+    PhiRefCell,
+    PhiRefValue
+);
+mesh.setFluxRequired(Phi.name());
+
+#include "createMRF.H"
+
+// Add overset specific interpolations
+{
+    dictionary oversetDict;
+    oversetDict.add("Phi", true);
+    oversetDict.add("U", true);
+
+    const_cast<dictionary&>
+    (
+        mesh.schemesDict()
+    ).add
+    (
+        "oversetInterpolationRequired",
+        oversetDict,
+        true
+    );
+}
+
+// Mask field for zeroing out contributions on hole cells
+#include "createCellMask.H"
+
+// Create bool field with interpolated cells
+#include "createInterpolatedCells.H"

applications/solvers/basic/potentialFoam/overPotentialFoam/potentialFoam.C

+/*---------------------------------------------------------------------------*\
+  =========                 |
+  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox
+   \\    /   O peration     |
+    \\  /    A nd           | Copyright (C) 2017 OpenCFD Ltd
+     \\/     M anipulation  |
+-------------------------------------------------------------------------------
+License
+    This file is part of OpenFOAM.
+
+    OpenFOAM is free software: you can redistribute it and/or modify it
+    under the terms of the GNU General Public License as published by
+    the Free Software Foundation, either version 3 of the License, or
+    (at your option) any later version.
+
+    OpenFOAM is distributed in the hope that it will be useful, but WITHOUT
+    ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
+    FITNESS FOR A PARTICULAR PURPOSE.  See the GNU General Public License
+    for more details.
+
+    You should have received a copy of the GNU General Public License
+    along with OpenFOAM.  If not, see <http://www.gnu.org/licenses/>.
+
+Application
+    potentialFoam
+
+Group
+    grpBasicSolvers
+
+Description
+    Potential flow solver which solves for the velocity potential, to
+    calculate the flux-field, from which the velocity field is obtained by
+    reconstructing the flux.
+
+    \heading Solver details
+    The potential flow solution is typically employed to generate initial fields
+    for full Navier-Stokes codes.  The flow is evolved using the equation:
+
+    \f[
+        \laplacian \Phi = \div(\vec{U})
+    \f]
+
+    Where:
+    \vartable
+        \Phi      | Velocity potential [m2/s]
+        \vec{U}   | Velocity [m/s]
+    \endvartable
+
+    The corresponding pressure field could be calculated from the divergence
+    of the Euler equation:
+
+    \f[
+        \laplacian p + \div(\div(\vec{U}\otimes\vec{U})) = 0
+    \f]
+
+    but this generates excessive pressure variation in regions of large
+    velocity gradient normal to the flow direction.  A better option is to
+    calculate the pressure field corresponding to velocity variation along the
+    stream-lines:
+
+    \f[
+        \laplacian p + \div(\vec{F}\cdot\div(\vec{U}\otimes\vec{U})) = 0
+    \f]
+    where the flow direction tensor \f$\vec{F}\f$ is obtained from
+    \f[
+        \vec{F} = \hat{\vec{U}}\otimes\hat{\vec{U}}
+    \f]
+
+    \heading Required fields
+    \plaintable
+        U         | Velocity [m/s]
+    \endplaintable
+
+    \heading Optional fields
+    \plaintable
+        p         | Kinematic pressure [m2/s2]
+        Phi       | Velocity potential [m2/s]
+                  | Generated from p (if present) or U if not present
+    \endplaintable
+
+    \heading Options
+    \plaintable
+        -writep   | write the Euler pressure
+        -writePhi | Write the final velocity potential
+        -initialiseUBCs | Update the velocity boundaries before solving for Phi
+    \endplaintable
+
+\*---------------------------------------------------------------------------*/
+
+#include "fvCFD.H"
+#include "pisoControl.H"
+#include "dynamicFvMesh.H"
+#include "cellCellStencilObject.H"
+#include "localMin.H"
+
+// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
+
+int main(int argc, char *argv[])
+{
+    argList::addOption
+    (
+        "pName",
+        "pName",
+        "Name of the pressure field"
+    );
+
+    argList::addBoolOption
+    (
+        "initialiseUBCs",
+        "Initialise U boundary conditions"
+    );
+
+    argList::addBoolOption
+    (
+        "writePhi",
+        "Write the final velocity potential field"
+    );
+
+    argList::addBoolOption
+    (
+        "writep",
+        "Calculate and write the Euler pressure field"
+    );
+
+    argList::addBoolOption
+    (
+        "withFunctionObjects",
+        "execute functionObjects"
+    );
+
+    #include "setRootCase.H"
+    #include "createTime.H"
+    #include "createNamedDynamicFvMesh.H"
+
+    pisoControl potentialFlow(mesh, "potentialFlow");
+
+    #include "createFields.H"
+
+    // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
+
+    Info<< nl << "Calculating potential flow" << endl;
+
+    mesh.update();
+
+    surfaceScalarField faceMask(localMin<scalar>(mesh).interpolate(cellMask));
+
+    // Since solver contains no time loop it would never execute
+    // function objects so do it ourselves
+    runTime.functionObjects().start();
+
+    MRF.makeRelative(phi);
+    adjustPhi(phi, U, p);
+
+    // Non-orthogonal velocity potential corrector loop
+    while (potentialFlow.correct())
+    {
+        phi = fvc::flux(U);
+
+        while (potentialFlow.correctNonOrthogonal())
+        {
+            fvScalarMatrix PhiEqn
+            (
+                fvm::laplacian(faceMask, Phi)
+            ==
+                fvc::div(phi)
+            );
+
+            PhiEqn.setReference(PhiRefCell, PhiRefValue);
+            PhiEqn.solve();
+
+            if (potentialFlow.finalNonOrthogonalIter())
+            {
+                phi -= PhiEqn.flux();
+            }
+        }
+
+        MRF.makeAbsolute(phi);
+
+        Info<< "Continuity error = "
+            << mag(fvc::div(phi))().weightedAverage(mesh.V()).value()
+            << endl;
+
+        U = fvc::reconstruct(phi);
+        U.correctBoundaryConditions();
+
+        Info<< "Interpolated velocity error = "
+            << (sqrt(sum(sqr(fvc::flux(U) - phi)))/sum(mesh.magSf())).value()
+            << endl;
+    }
+
+    // Write U and phi
+    U.write();
+    phi.write();
+
+    // Optionally write Phi
+    if (args.optionFound("writePhi"))
+    {
+        Phi.write();
+    }
+
+    // Calculate the pressure field from the Euler equation
+    if (args.optionFound("writep"))
+    {
+        Info<< nl << "Calculating approximate pressure field" << endl;
+
+        label pRefCell = 0;
+        scalar pRefValue = 0.0;
+        setRefCell
+        (
+            p,
+            potentialFlow.dict(),
+            pRefCell,
+            pRefValue
+        );
+
+        // Calculate the flow-direction filter tensor
+        volScalarField magSqrU(magSqr(U));
+        volSymmTensorField F(sqr(U)/(magSqrU + SMALL*average(magSqrU)));
+
+        // Calculate the divergence of the flow-direction filtered div(U*U)
+        // Filtering with the flow-direction generates a more reasonable
+        // pressure distribution in regions of high velocity gradient in the
+        // direction of the flow
+        volScalarField divDivUU
+        (
+            fvc::div
+            (
+                F & fvc::div(phi, U),
+                "div(div(phi,U))"
+            )
+        );
+
+        // Solve a Poisson equation for the approximate pressure
+        while (potentialFlow.correctNonOrthogonal())
+        {
+            fvScalarMatrix pEqn
+            (
+                fvm::laplacian(p) + divDivUU
+            );
+
+            pEqn.setReference(pRefCell, pRefValue);
+            pEqn.solve();
+        }
+
+        p.write();
+    }
+
+    runTime.functionObjects().end();
+
+    Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
+        << "  ClockTime = " << runTime.elapsedClockTime() << " s"
+        << nl << endl;
+
+    Info<< "End\n" << endl;
+
+    return 0;
+}
+
+
+// ************************************************************************* //

applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/Make/files

+rhoSimpleFoam.C
+
+EXE = $(FOAM_APPBIN)/overRhoSimpleFoam

applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/Make/options

+EXE_INC = \
+    -I.. \
+    -I$(LIB_SRC)/transportModels/compressible/lnInclude \
+    -I$(LIB_SRC)/thermophysicalModels/basic/lnInclude \
+    -I$(LIB_SRC)/TurbulenceModels/turbulenceModels/lnInclude \
+    -I$(LIB_SRC)/TurbulenceModels/compressible/lnInclude \
+    -I$(LIB_SRC)/finiteVolume/cfdTools \
+    -I$(LIB_SRC)/finiteVolume/lnInclude \
+    -I$(LIB_SRC)/sampling/lnInclude \
+    -I$(LIB_SRC)/dynamicFvMesh/lnInclude \
+    -I$(LIB_SRC)/dynamicMesh/lnInclude \
+    -I$(LIB_SRC)/meshTools/lnInclude \
+    -I$(LIB_SRC)/overset/lnInclude
+
+EXE_LIBS = \
+    -lcompressibleTransportModels \
+    -lfluidThermophysicalModels \
+    -lspecie \
+    -lturbulenceModels \
+    -lcompressibleTurbulenceModels \
+    -lfiniteVolume \
+    -lsampling \
+    -lmeshTools \
+    -lfvOptions \
+    -loverset \
+    -ldynamicFvMesh \
+    -ltopoChangerFvMesh

applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/UEqn.H

+    // Solve the Momentum equation
+    MRF.correctBoundaryVelocity(U);
+
+    tmp<fvVectorMatrix> tUEqn
+    (
+        fvm::div(phi, U)
+      + MRF.DDt(rho, U)
+      + turbulence->divDevRhoReff(U)
+     ==
+        fvOptions(rho, U)
+    );
+    fvVectorMatrix& UEqn = tUEqn.ref();
+
+    UEqn.relax();
+
+    fvOptions.constrain(UEqn);
+
+    if (simple.momentumPredictor())
+    {
+        solve(UEqn == -cellMask*fvc::grad(p));
+    }
+
+    fvOptions.correct(U);

applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/createFieldRefs.H

+const volScalarField& psi = thermo.psi();

applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/createFields.H

+Info<< "Reading thermophysical properties\n" << endl;
+
+autoPtr<fluidThermo> pThermo
+(
+    fluidThermo::New(mesh)
+);
+fluidThermo& thermo = pThermo();
+thermo.validate(args.executable(), "h", "e");
+
+volScalarField& p = thermo.p();
+
+volScalarField rho
+(
+    IOobject
+    (
+        "rho",
+        runTime.timeName(),
+        mesh,
+        IOobject::READ_IF_PRESENT,
+        IOobject::AUTO_WRITE
+    ),
+    thermo.rho()
+);
+
+Info<< "Reading field U\n" << endl;
+volVectorField U
+(
+    IOobject
+    (
+        "U",
+        runTime.timeName(),
+        mesh,
+        IOobject::MUST_READ,
+        IOobject::AUTO_WRITE
+    ),
+    mesh
+);
+
+#include "compressibleCreatePhi.H"
+
+pressureControl pressureControl(p, rho, simple.dict());
+
+mesh.setFluxRequired(p.name());
+
+Info<< "Creating turbulence model\n" << endl;
+autoPtr<compressible::turbulenceModel> turbulence
+(
+    compressible::turbulenceModel::New
+    (
+        rho,
+        U,
+        phi,
+        thermo
+    )
+);
+
+dimensionedScalar initialMass = fvc::domainIntegrate(rho);
+
+#include "createMRF.H"
+
+//- Overset specific
+
+// Add solver-specific interpolations
+{
+    dictionary oversetDict;
+    oversetDict.add("U", true);
+    oversetDict.add("p", true);
+    oversetDict.add("HbyA", true);
+    oversetDict.add("grad(p)", true);
+    oversetDict.add("rho", true);
+
+    const_cast<dictionary&>
+    (
+        mesh.schemesDict()
+    ).add
+    (
+        "oversetInterpolationRequired",
+        oversetDict,
+        true
+    );
+}
+
+// Mask field for zeroing out contributions on hole cells
+#include "createCellMask.H"
+
+#include "createInterpolatedCells.H"
+
+bool adjustFringe
+(
+    simple.dict().lookupOrDefault("oversetAdjustPhi", false)
+);

applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/createUpdatedDynamicFvMesh.H

+    Info<< "Create dynamic mesh for time = "
+        << runTime.timeName() << nl << endl;
+
+    autoPtr<dynamicFvMesh> meshPtr
+    (
+        dynamicFvMesh::New
+        (
+            IOobject
+            (
+                dynamicFvMesh::defaultRegion,
+                runTime.timeName(),
+                runTime,
+                IOobject::MUST_READ
+            )
+        )
+    );
+
+    dynamicFvMesh& mesh = meshPtr();
+
+    // Calculate initial mesh-to-mesh mapping. Note that this should be
+    // done under the hood, e.g. as a MeshObject
+    mesh.update();

applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/pEqn.H

+{
+    surfaceScalarField faceMask(localMin<scalar>(mesh).interpolate(cellMask));
+
+    volScalarField rAU(1.0/UEqn.A());
+    surfaceScalarField rhorAUf("rhorAUf", faceMask*fvc::interpolate(rho*rAU));
+    volVectorField HbyA("HbyA", U);
+    HbyA = constrainHbyA(cellMask*rAU*UEqn.H(), U, p);
+    tUEqn.clear();
+
+    bool closedVolume = false;
+
+    surfaceScalarField phiHbyA("phiHbyA", fvc::interpolate(rho)*fvc::flux(HbyA));
+    MRF.makeRelative(fvc::interpolate(rho), phiHbyA);
+
+    // Update the pressure BCs to ensure flux consistency
+    constrainPressure(p, rho, U, phiHbyA, rhorAUf, MRF);
+
+    if (simple.transonic())
+    {
+        surfaceScalarField phid
+        (
+            "phid",
+            (fvc::interpolate(psi)/fvc::interpolate(rho))*phiHbyA
+        );
+
+        phiHbyA -= fvc::interpolate(psi*p)*phiHbyA/fvc::interpolate(rho);
+
+        while (simple.correctNonOrthogonal())
+        {
+            fvScalarMatrix pEqn
+            (
+                fvc::div(phiHbyA)
+              + fvm::div(phid, p)
+              - fvm::laplacian(rhorAUf, p)
+            ==
+                fvOptions(psi, p, rho.name())
+            );
+
+            // Relax the pressure equation to ensure diagonal-dominance
+            pEqn.relax();
+
+            pEqn.setReference
+            (
+                pressureControl.refCell(),
+                pressureControl.refValue()
+            );
+
+            pEqn.solve();
+
+            if (simple.finalNonOrthogonalIter())
+            {
+                phi = phiHbyA + pEqn.flux();
+            }
+        }
+    }
+    else
+    {
+        closedVolume = adjustPhi(phiHbyA, U, p);
+
+        if (adjustFringe)
+        {
+            oversetAdjustPhi(phiHbyA, U);
+        }
+
+        while (simple.correctNonOrthogonal())
+        {
+            fvScalarMatrix pEqn
+            (
+                fvc::div(phiHbyA)
+              - fvm::laplacian(rhorAUf, p)
+            ==
+                fvOptions(psi, p, rho.name())
+            );
+
+            pEqn.setReference
+            (
+                pressureControl.refCell(),
+                pressureControl.refValue()
+            );
+
+            pEqn.solve();
+
+            if (simple.finalNonOrthogonalIter())
+            {
+                phi = phiHbyA + pEqn.flux();
+            }
+        }
+    }
+
+    #include "incompressible/continuityErrs.H"
+
+    // Explicitly relax pressure for momentum corrector
+    p.relax();
+
+    volVectorField gradP(fvc::grad(p));
+
+    U = HbyA - rAU*cellMask*gradP;
+    U.correctBoundaryConditions();
+    fvOptions.correct(U);
+
+
+    bool pLimited = pressureControl.limit(p);
+
+    // For closed-volume cases adjust the pressure and density levels
+    // to obey overall mass continuity
+    if (closedVolume)
+    {
+        p += (initialMass - fvc::domainIntegrate(psi*p))
+            /fvc::domainIntegrate(psi);
+    }
+
+    if (pLimited || closedVolume)
+    {
+        p.correctBoundaryConditions();
+    }
+
+    rho = thermo.rho();
+
+    if (!simple.transonic())
+    {
+        rho.relax();
+    }
+}

applications/solvers/compressible/rhoSimpleFoam/overRhoSimpleFoam/rhoSimpleFoam.C

+/*---------------------------------------------------------------------------*\
+  =========                 |
+  \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox
+   \\    /   O peration     |
+    \\  /    A nd           | Copyright (C) 2017 OpenCFD Ltd
+     \\/     M anipulation  |
+-------------------------------------------------------------------------------
+License
+    This file is part of OpenFOAM.
+
+    OpenFOAM is free software: you can redistribute it and/or modify it
+    under the terms of the GNU General Public License as published by
+    the Free Software Foundation, either version 3 of the License, or
+    (at your option) any later version.
+
+    OpenFOAM is distributed in the hope that it will be useful, but WITHOUT
+    ANY WARRANTY; without even the implied warranty of MERCHANTABILITY or
+    FITNESS FOR A PARTICULAR PURPOSE.  See the GNU General Public License
+    for more details.
+
+    You should have received a copy of the GNU General Public License
+    along with OpenFOAM.  If not, see <http://www.gnu.org/licenses/>.
+
+Application
+    overRhoSimpleFoam
+
+Group
+    grpCompressibleSolvers
+
+Description
+    Overset steady-state solver for turbulent flow of compressible fluids.
+
+\*---------------------------------------------------------------------------*/
+
+#include "fvCFD.H"
+#include "dynamicFvMesh.H"
+#include "fluidThermo.H"
+#include "turbulentFluidThermoModel.H"
+#include "simpleControl.H"
+#include "pressureControl.H"
+#include "fvOptions.H"
+#include "cellCellStencilObject.H"
+#include "localMin.H"
+#include "oversetAdjustPhi.H"
+
+// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
+
+int main(int argc, char *argv[])
+{
+    #define CREATE_MESH createUpdatedDynamicFvMesh.H
+    #include "postProcess.H"
+
+    #include "setRootCase.H"
+    #include "createTime.H"
+    #include "createUpdatedDynamicFvMesh.H"
+    #include "createControl.H"
+    #include "createFields.H"
+    #include "createFieldRefs.H"
+    #include "createFvOptions.H"
+    #include "initContinuityErrs.H"
+
+    turbulence->validate();
+
+    // * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
+
+    Info<< "\nStarting time loop\n" << endl;
+
+    while (simple.loop())
+    {
+        Info<< "Time = " << runTime.timeName() << nl << endl;
+
+        // Pressure-velocity SIMPLE corrector
+        #include "UEqn.H"
+        #include "EEqn.H"
+        #include "pEqn.H"
+
+        turbulence->correct();
+
+        runTime.write();
+
+        Info<< "ExecutionTime = " << runTime.elapsedCpuTime() << " s"
+            << "  ClockTime = " << runTime.elapsedClockTime() << " s"
+            << nl << endl;
+    }
+
+    Info<< "End\n" << endl;
+
+    return 0;
+}
+
+
+// ************************************************************************* //

tutorials/basic/overPotentialFoam/cylinder/Allclean

+#!/bin/sh
+cd ${0%/*} || exit 1    # run from this directory
+. $WM_PROJECT_DIR/bin/tools/CleanFunctions
+
+# Extrude mesh around cylinder
+(cd cylinderAndBackground && ./Allclean)
+
+# Add background mesh
+(cd cylinderMesh && foamCleanTutorials)
+
+# ----------------------------------------------------------------- end-of-file

tutorials/basic/overPotentialFoam/cylinder/Allrun

+#!/bin/sh
+. $WM_PROJECT_DIR/bin/tools/RunFunctions
+
+# Extrude mesh around cylinder
+(cd cylinderMesh && ./Allrun.pre)
+
+# Add background mesh
+(cd cylinderAndBackground && ./Allrun)

tutorials/basic/overPotentialFoam/cylinder/Allrun.pre

+#!/bin/sh
+. $WM_PROJECT_DIR/bin/tools/RunFunctions
+
+# Extrude mesh around cylinder
+(cd cylinderMesh && ./Allrun.pre)
+
+# Add background mesh
+(cd cylinderAndBackground && ./Allrun.pre)

tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/0.orig/U

+/*--------------------------------*- C++ -*----------------------------------*\
+| =========                 |                                                 |
+| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
+|  \\    /   O peration     | Version:  plus                                  |
+|   \\  /    A nd           | Web:      www.OpenFOAM.com                      |
+|    \\/     M anipulation  |                                                 |
+\*---------------------------------------------------------------------------*/
+FoamFile
+{
+    version     2.0;
+    format      ascii;
+    class       volVectorField;
+    object      U;
+}
+// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
+
+#include        "include/initialConditions"
+
+dimensions      [0 1 -1 0 0 0 0];
+
+internalField   uniform $flowVelocity;
+
+boundaryField
+{
+    #includeEtc "caseDicts/setConstraintTypes"
+
+    overset
+    {
+        type            overset;
+    }
+
+    walls
+    {
+        type            movingWallVelocity;
+        value           uniform (0 0 0);
+    }
+
+    inlet
+    {
+        type            fixedValue;
+        value           $internalField;
+    }
+
+    outlet
+    {
+        type            inletOutlet;
+        inletValue      uniform (0 0 0);
+        value           $internalField;
+    }
+
+    topAndBottom
+    {
+        type            zeroGradient;
+    }
+}
+
+// ************************************************************************* //

tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/0.orig/include/fixedInlet

+/*--------------------------------*- C++ -*----------------------------------*\
+| =========                 |                                                 |
+| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
+|  \\    /   O peration     | Version:  plus                                  |
+|   \\  /    A nd           | Web:      www.OpenFOAM.com                      |
+|    \\/     M anipulation  |                                                 |
+\*---------------------------------------------------------------------------*/
+
+inlet
+{
+    type  fixedValue;
+    value $internalField;
+}
+
+// ************************************************************************* //

tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/0.orig/include/initialConditions

+/*--------------------------------*- C++ -*----------------------------------*\
+| =========                 |                                                 |
+| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
+|  \\    /   O peration     | Version:  plus                                  |
+|   \\  /    A nd           | Web:      www.OpenFOAM.com                      |
+|    \\/     M anipulation  |                                                 |
+\*---------------------------------------------------------------------------*/
+
+flowVelocity         (1 0 0);
+pressure             0;
+#inputMode           merge
+
+// ************************************************************************* //

tutorials/basic/overPotentialFoam/cylinder/cylinderAndBackground/0.orig/p

+/*--------------------------------*- C++ -*----------------------------------*\
+| =========                 |                                                 |
+| \\      /  F ield         | OpenFOAM: The Open Source CFD Toolbox           |
+|  \\    /   O peration     | Version:  plus                                  |
+|   \\  /    A nd           | Web:      www.OpenFOAM.com                      |
+|    \\/     M anipulation  |                                                 |
+\*---------------------------------------------------------------------------*/
+FoamFile
+{
+    version     2.0;
+    format      ascii;
+    class       volScalarField;
+    object      p;
+}
+// * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * * //
+
+#include        "include/initialConditions"
+
+dimensions      [0 2 -2 0 0 0 0];
+
+internalField   uniform $pressure;
+
+boundaryField
+{
+    #includeEtc "caseDicts/setConstraintTypes"
+
+    overset
+    {
+        type            overset;
+    }
+
+    wall
+    {
+        type            zeroGradient;
+    }
+
+    inlet
+    {
+        type            zeroGradient;
+    }
+
+    outlet
+    {
+        type            fixedValue;   //calculated;
+        value           $internalField;
+    }
+
+    ".*"
+    {
+        type            zeroGradient;
+    }
+}
+
+// ************************************************************************* //